AD 96-06-11

final rule
Data completeness: 70%

Airworthiness Directives; AlliedSignal Inc. TPE331 Series Turboprop Engines

AD Number
96-06-11
Status
final_rule
Effective Date
Product Category
engine
Docket
95-ANE-09
FR Citation
Federal Register: March 26, 1996 (Volume 61, Number 59)

Applicability

TypeManufacturerModelDetails
engine Honeywell International Inc. TPE331-14A Airworthiness Directives; AlliedSignal Inc. TPE331 Series Turboprop Engines
engine Honeywell International Inc. TPE331-14B Airworthiness Directives; AlliedSignal Inc. TPE331 Series Turboprop Engines
engine Honeywell International Inc. TPE331-14F Airworthiness Directives; AlliedSignal Inc. TPE331 Series Turboprop Engines
engine Honeywell International Inc. TPE331-15AW Airworthiness Directives; AlliedSignal Inc. TPE331 Series Turboprop Engines

Unsafe Condition

Fatigue failure of engine compressor components (main shouldered shafts and forward coupling shafts) due to accumulative cyclic effects without an established retirement life, leading to an inflight engine shutdown.

AI-generated summary from the source AD text. Verify against the official source before acting.

Required Actions

Initiate life limited part log cards for main shouldered shafts and forward coupling shafts. Remove main shouldered shafts from service based on cycles in service (5,600 or less CIS prior to 6,000 CIS or within 400 CIS after AD effective date if over 5,600 CIS). Remove forward coupling shafts prior to 20,000 CIS at next major inspection or compressor disassembly after AD effective date. Actions must follow specified AlliedSignal service documents.

AI-generated summary from the source AD text. Verify against the official source before acting.

Compliance Time

Required as indicated, unless accomplished previously.

AI-generated summary from the source AD text. Verify against the official source before acting.

Affected Aircraft

AlliedSignal Inc. (formerly Garrett Engine Division) Models TPE331-14A, -14B, -14F, and -15AW turboprop engines installed on Piper Model PA-42-1000 and Grumman Model TS-2A (modified per STC SA4837NM).

AI-generated summary from the source AD text. Verify against the official source before acting.

Source: Official FAA Source ↗

Retrieved: Apr 8, 2026

Rights: U.S. Government Public Domain

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